2020
DOI: 10.1007/s41810-020-00071-5
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A User-Centric Design Thinking Approach for Advancement in Off-Line PM Air Samplers: Current Status and Future Directions

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Cited by 1 publication
(3 citation statements)
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“…Compared to turboramjet engines, they have a lower weight and smaller sizes. However, the low fuel economy made it more suitable for short-duration aircraft in the space-launcher type where high speed and altitude performance is critical [11].…”
Section: Turborocketmentioning
confidence: 99%
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“…Compared to turboramjet engines, they have a lower weight and smaller sizes. However, the low fuel economy made it more suitable for short-duration aircraft in the space-launcher type where high speed and altitude performance is critical [11].…”
Section: Turborocketmentioning
confidence: 99%
“…Jet engines are required to provide high performance under different operating conditions, such as high ambiance temperature, heavy rain, strong wind and snow. The engine selection criteria base on aircraft size, flight range, speed, aerodynamics behaviour and operation way [11]. However, each factor could pull the engine design in a different direction.…”
Section: Civil Transportmentioning
confidence: 99%
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